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How to calculate the AoA (Euler angles) in 6DOF model?

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August 27, 2014, 06:16	How to calculate the AoA (Euler angles) in 6DOF model?	#1
jiec827 New Member Cheng Jie Join Date: Nov 2011 Posts: 8 Rep Power: 15	Hi Foamers, Now I am simulating a case with sixDoF dynamic mesh model (similar to FOAM_TUTORIALS/incompressible/pimpleDyMFoam/wingMotion/wingMotion2D_pimpleDyMFoam). During the post-process, all I want is the curves between Angle of Attack and lift coefficient. But I have no idea about how to calculate the AoA in this kind of aero-actuated model. Does any one have any experiences? Jie

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